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# Transfer Function Notes | EduRev

## Electrical Engineering (EE) : Transfer Function Notes | EduRev

The document Transfer Function Notes | EduRev is a part of the Electrical Engineering (EE) Course Control Systems.
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Transfer Function

The Transfer Function (TF) of a System is the ratio of the output to the input of a system, in the Laplace domain considering its initial conditions and equilibrium point to be zero.
If we have an input function of X(s), and an output function Y(s), we deﬁne the transfer function H(s).
H(s) = Y(s)/X(s)

Impulse Response

Since we know that in the time domain, generally, we define the input to a system as x(t), and the output of the system as y(t). The relationship between the input and the output is represented as the impulse response, h(t).
We can use the following equation to deﬁne the impulse response:
h(t) = y(t) / x(t)

• The Impulse Function, denoted with δ(t) is a function deﬁned piece-wise as follows
• An examination of the impulse function shows that it is related to the unit-step function as follows
u(t) = ∫δ(t) or δ(t) = du(t) / dt
• The impulse response (IR) must always satisfy the following condition, or else it is not a true impulse function

Convolution in Time Domain

If we have the system input and the impulse response of the system, we can calculate the system output using the convolution operation as such as
y(t) = h(t) ∗ x(t).

Time-Invariant System Response

• If the system is time-invariant, then the general description of the system can be replaced by a convolution integral of the system's impulse response and the system input. We can call this the convolution description of a system.

Convolution Theorem

• Convolution in the time domain turns into multiplication in the complex Laplace domain.
• Multiplication in the time domain turns into convolution in the complex Laplace domain.
L[f(t) ∗ g(t)] = F(s)G(s)
L[f(t)g(t)] = F(s) ∗ G(s)
Result: If the complex Laplace variable is s, then we generally denote the transfer function of a system as either G(s) or H(s). If the system input is X(s), and the system output is Y(s), then the transfer function can be deﬁned as such
H(s) = Y(s)/X(s)
• So if we know the input to a given system, and we have the transfer function of the system, we can solve for the system output by multiplying as
Y(s) = H(s)X(s)

Example: Impulse Response

• Since we know that the Laplace transform of the impulse function, δ(t) is L[δ(t)] = 1
• So, when we put this into the relationship between the input, output, and transfer function, we get
Y(s) = X(s)H(s)
or Y(s) = (1)H(s)
or Y(s) = H(s)
In other words, the "impulse response" is the o/p of the system when we input an impulse function.

Transfer Functions for Linear Systems

Consider a linear input/output system described by the controlled differential equation

where u is the input and y are the output.

• To obtain the transfer function of the system of last equation let us input be u(t) = est.
• Since the system is linear, there is an output of the system that is also an exponential function  ⇒ y(t) = Yoest
• Inserting the signals into last equation ,we ﬁnd
(sn + a1sn−1 +···+ an)yo.est = (bosm + b1sm−1···+ bm)e−st
• And the response of the system can be completely described as
a(s) = sn + a1sn−1 +···+ an &  b(s) = bosm + b1sm−1 + ···+ bm
y(t) = y0est = (b(s) / a(s))est
• So the transfer function of the given function is given by
G(s) = b(s) / a(s)

Transfer Function Alternative Method

To investigate how a linear system responds to the exponential input u(t) = est we consider the state space system
dx/dt = Ax + Bu
y = Cx + Du
Let the input signal be u(t) = est and assume that s ≠ λi(A),  where i = 1,...,n, where λi(A) is the ith eigenvalue of A. then

Since s ≠ λ(A) the integral can be evaluated and we get

& Output y(t) = Cx(t) + Du(t)
= CeAt{x(0) − (sI − A)−1B} + [D + C(sI − A)−1B]est
Note: One term of the output is proportional to the input u(t) = est. This term is called the pure exponential response.

• If the initial state is chosen as x(0) = (sI −A)−1B
• the output only consists of the only exponential response and both the state and the output are directly proportional to the input
x(t) = (sI − A)−1Best = (sI − A)−1Bu(t)
y(t) = [C(sI − A)−1B+D]est = [C(sI − A)−1B + D]u(t).
• The ratio of the output and the input
G(s) = C(sI − A)−1B + D is the transfer function of the system.
• For Homogeneous Equation i.e; D = 0 then
G(s) = C(sI − A)−1B  is the transfer function of the system.

The Concept of Pole & Zero

• Poles and Zeros of a transfer function are the frequencies for which the value of the transfer function becomes inﬁnity or zero respectively.
• The transfer function has many useful explanations and the features of a transfer function are often associated with important system properties. Three of the most important features are the gain and the locations of the poles and zeros.
H(s) = N(s)/D(s)
• In the above equation, N(s) and D(s) are simple polynomials in s. Zeros are the roots of N(s) by setting N(s) = 0 and solving for s. Poles are the roots of D(s), by setting D(s) = 0 and solving for s.
• In general Transfer Function must not have more zeros than poles, we can state that the polynomial order of D(s) must be greater than or equal to the polynomial order of N(s).

Eﬀects of Poles and Zeros

• when s approaches a zero (Zeros of Transfer function), the numerator of the transfer function N(s)→0.
• When s approaches a pole (Poles of Transfer Function) the denominator of the transfer function D(s)→0 & the value of the transfer function approaches inﬁnity.
• An output value of inﬁnity should raise an alarm bell for people who are familiar with BIBO stability.
• Poles & Zeros of a transfer function are represented in S-Plane, In s-plane s = σ ± jω  where σ represent the attenuation on X-axis & ω  represents the angular velocity represented on the y-axis.
• In s-plane, the Poles are located by a cross (*) & the Zeros are located by dot (.)
• For a Stable System, All the Poles & Zeros of a Transfer Function must be lie in the left half of s-plane.

Note: If the Poles or Zero lie on the imaginary axis then it must be simple (order only 1) then the system is said to be Marginally Stable, If the Order of multiplicity of Poles or Zeros on Imaginary Axis is more than 1 in that case system will become Unstable.

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